Reheating in a gas turbine Increases the compressor work Increases the thermal efficiency Decreases the thermal efficiency Increases the turbine work TRUE ANSWER : ? YOUR ANSWER : ?
Propulsion efficiency of the following order is obtained in practice 0.5 0.34 0.6 0.72 TRUE ANSWER : ? YOUR ANSWER : ?
Axial flow compressor has the following advantage over centrifugal compressor Higher pressure ratio per stage Larger air handling ability per unit frontal area Higher average velocities Aerofoil blades are used TRUE ANSWER : ? YOUR ANSWER : ?
Work ratio of a gas turbine may be improved by Increasing the compression work Decreasing the compression work Increasing the turbine work Both (A) and (C) above TRUE ANSWER : ? YOUR ANSWER : ?
Ratio of indicated h.p. to shaft h.p. in known as Isothermal efficiency Volumetric efficiency Compressor efficiency Mechanical efficiency TRUE ANSWER : ? YOUR ANSWER : ?
Gas turbine works on Ericsson cycle Carnot cycle Rankine cycle Brayton or Atkinson cycle TRUE ANSWER : ? YOUR ANSWER : ?
If p₁, is the pressure of air entering the L.P. cylinder and p₂ is the pressure of air leaving the L.P. cylinder (or inter-cooler pressure), then the ratio of cylinder diameters for a single acting, two stage reciprocating air compressor with complete intercooling is given by (where D₁ = Dia. of L.P. cylinder, and D₂ = Dia. of H.P. cylinder) D₁/D₂ = p₂/p₁ D₁/D₂ = p₁/p₂ D₁/D₂ = p₁ p₂ None of these TRUE ANSWER : ? YOUR ANSWER : ?
The work ratio of simple gas turbine cycle depends on Maximum cycle temperature Minimum cycle temperature All of these Pressure ratio TRUE ANSWER : ? YOUR ANSWER : ?
In a jet engine, the air-fuel ratio is 2.0840277777778 2.5006944444444 1.6673611111111 1.2506944444444 TRUE ANSWER : ? YOUR ANSWER : ?
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio Decreases Increases First decreases and then increases First increases and then decreases TRUE ANSWER : ? YOUR ANSWER : ?